鼓泡箔片动压气体径向轴承库仑阻尼耗散的数值分析

赵琪; 侯予; 任雄豪; 陈双涛; 赖天伟

doi:10.7652/xjtuxb202110017

您当前的位置：

首页 >

文章列表页 >

鼓泡箔片动压气体径向轴承库仑阻尼耗散的数值分析

更新时间：2025-07-09

- 鼓泡箔片动压气体径向轴承库仑阻尼耗散的数值分析
- Numerical Analysis of Coulomb Damping Dissipation of Protuberant Gas Foil Journal Bearing
- 西安交通大学学报 2021年55卷第10期页码：150-156
- 作者机构：
  
  西安交通大学能源与动力工程学院,西安,710049
- 作者简介：
  
  赖天伟(通信作者),男,副教授,博士生导师。基金项目: 国家重点研发计划资助项目(2019YFB1504600)
- 基金信息：
  
  : 2020-12-14。作者简介: 赵琪(1995—),男,硕士生;赖天伟(通信作者),男,副教授,博士生导师。基金项目: 国家重点研发计划资助项目(2018YFB2000100);国家自然科学基金资助项目(51976150);陕西高校青年创新团队资助项目
- DOI：10.7652/xjtuxb202110017
  中图分类号： TH133
- 网络首发：2021-10-10，
  
  纸质出版：2021
- 稿件说明：
移动端阅览
赵琪, 侯予, 任雄豪, 等. 鼓泡箔片动压气体径向轴承库仑阻尼耗散的数值分析[J]. 西安交通大学学报, 2021,55(10):150-156.

Numerical Analysis of Coulomb Damping Dissipation of Protuberant Gas Foil Journal Bearing[J]. 2021, 55(10): 150-156.
赵琪, 侯予, 任雄豪, 等. 鼓泡箔片动压气体径向轴承库仑阻尼耗散的数值分析[J]. 西安交通大学学报, 2021,55(10):150-156. DOI： 10.7652/xjtuxb202110017.

Numerical Analysis of Coulomb Damping Dissipation of Protuberant Gas Foil Journal Bearing[J]. 2021, 55(10): 150-156. DOI： 10.7652/xjtuxb202110017.

摘要

为了更好地研究箔片轴承的动态特性和稳定性

提高高速透平机械中轴承转子的系统稳定性

采用能量耗散的方法对单层和双层鼓泡箔片轴承的库仑阻尼耗散能量进行了分析与评价

获得了箔片厚度、周向和轴向鼓泡支承点间距等结构参数以及弹性模量对库仑阻尼耗散能量的影响。数值研究结果表明:随着箔片厚度的减小

周向鼓泡间距减小

库仑阻尼耗散能量增加; 轴向鼓泡支承点密度增大以及偏心率和转速的升高也会加强库仑阻尼耗散; 在相同工况下

双层鼓泡箔片轴承的库仑阻尼耗散明显大于单层鼓泡箔片轴承

且改变双层鼓泡箔片轴承中层鼓泡箔片厚度耗散能量效果优于改变顶层平箔厚度; 高弹性模量材料的硬度高

箔片滑移量小

会减小库仑阻尼耗散能量; 相同条件下

鼓泡箔片轴承选用高弹性模量材料时库仑阻尼耗散能量更小。

Abstract

In order to better study the dynamic characteristics and stability of gas foil bearings and improve the stability of the rotor bearing system in high-speed turbomachinery

the energy dissipation method is used to analyze and evaluate the dissipation energy of Coulomb damping in single and double protuberant foil bearings. The influences of foil thickness

circumferential and axial protuberant pitch and elastic modulus on the dissipation energy of Coulomb damping are obtained. Numerical results show that the energy dissipated by Coulomb damping increases with the decrease of foil thickness and the decrease of the circumferential protuberant pitch. The Coulomb damping dissipated energy is enlarged by increasing the density of axial protuberant points and the increase of eccentricity and rotate speeds. The Coulomb damping dissipation effect of double-layer protuberant foil bearing is significantly greater than that of single-layer protuberant foil bearing under the same working condition. Moreover

the effect of changing the thickness of the middle protuberant foil to dissipate energy is better than that of changing the thickness of the top layer flat foil. The material foil with high elastic modulus has higher hardness and less slippage

which would reduce the energy dissipation of Coulomb damping. Less energy is dissipated through Coulomb damping when the protuberant foil bearing is made of materials with high elastic modulus under the same conditions.

关键词

Keywords

references

郭雨, 赖天伟, 赵琪, 等. 悬臂型箔片轴承应用于高速透平的实验研究 [J]. 西安交通大学学报, 2020, 54(5): 40-45.

GUO Yu, LAI Tianwei, ZHAO Qi, et al. Experimental study of multi-leaf foil bearing in high-speed turbo-machinery [J]. Journal of Xi'an Jiaotong University, 2020, 54(5): 40-45.

SAMANTA P, MURMU N C, KHONSARI M M. The evolution of foil bearing technology [J]. Tribology International, 2019, 135: 305-323.

SIM K, LEE Y B, KIM T H. Rotordynamic analysis of an oil-free turbocharger supported on lobed gas foil bearings: predictions versus test data [J]. Tribology Transactions, 2014, 57(6): 1086-1095.

绳春晨, 杨榆, 谢洪涛, 等. 箔片动压轴承的研制及在机载环控涡轮的应用 [J]. 润滑与密封, 2020, 45(5): 86-90.

SHENG Chunchen, YANG Yu, XIE Hongtao, et al. Development and application of aerodynamic foil bearings in high-speed turbo-machinery of airborne ECS [J]. Lubrication Engineering, 2020, 45(5): 86-90.

AGRAWALI G L. Foil air/gas bearing technology: an overview [C]∥Proceedings of the ASME 1997 International Gas Turbine and Aeroengine Congress and Exhibition. New York, USA: ASME, 1997: V001T 04A006.

ZHENG Yueqing, CHEN Shuangtao, LAI Tianwei, et al. Numerical and experimental study on the dynamic characteristics of the foil journal bearing with double-layer protuberant support [J]. Journal of Advanced Mechanical Design Systems and Manufacturing, 2016, 10(2): 0027.

王林忠, 侯予, 崔明现, 等. 影响箔片结构阻尼的因素及箔片径向轴承结构形式的进展 [J]. 润滑与密封, 2006, 31(1): 139-142, 146.

WANG Linzhong, HOU Yu, CUI Mingxian, et al. Effects on the damping of foil journal bearings and the development of the foil structure [J]. Lubrication Engineering, 2006, 31(1): 139-142, 146.

赖天伟, 马斌, 郑越青, 等. 多层弹性支承箔片动压气体径向轴承稳定性的实验研究 [J]. 西安交通大学学报, 2014, 48(3): 79-83.

LAI Tianwei, MA Bin, ZHENG Yueqing, et al. Experimental investigation on stability of multi-decked protuberant foil gas journal bearing [J]. Journal of Xi'an Jiaotong University, 2014, 48(3): 79-83.

WA L J A, ANNO J N, HAMROCK B J. Modern developments in lubrication mechanics [J]. Tribology International, 1977, 9(2): 90.

徐方程, 刘占生, 张广辉, 等. 箔片结构库仑摩擦效应对径向箔片轴承特性的影响 [J]. 航空动力学报, 2013, 28(8): 1865-1874.

XU Fangcheng, LIU Zhansheng, ZHANG Guanghui, et al. Effects of Coulomb friction in foil structure on foil journal bearing performance [J]. Journal of Aerospace Power, 2013, 28(8): 1865-1874.

ZYWICA G, BAGINSKI P, BOGULICZ M. Experimental and numerical evaluation of the damping properties of a foil bearing structure taking into account the static and kinetic dry friction [J]. Journal of the Brazilian Society of Mechanical Sciences and Engineering, 2020, 43(1): 1-23.

ARGHIR M, BENCHEKROUN O. A simplified structural model of bump-type foil bearings based on contact mechanics including gaps and friction [J]. Tribology International, 2019, 134: 129-144.

HOU Yu, CHEN Shuangtao, CHEN Rugang, et al. Numerical study on foil journal bearings with protuberant foil structure [J]. Tribology International, 2011, 44(9): 1061-1070.

赖天伟, 郑越青, 陈双涛, 等. 多层鼓泡弹性支承箔片动压气体轴承的实验研究 [J]. 东北大学学报(自然科学版), 2014, 35(3): 415-418.

LAI Tianwei, ZHENG Yueqing, CHEN Shuangtao, et al. Experimental study on the performance of multi-decked elastic support protuberant foil gas bearing [J]. Journal of Northeastern University(Natural Science), 2014, 35(3): 415-418.

周权, 侯予, 陈汝刚. 应用于高速透平膨胀机的箔片动压气体止推轴承的试验研究 [J]. 西安交通大学学报, 2012, 46(11): 49-52, 111.

ZHOU Quan, HOU Yu, CHEN Rugang. Experimental research on compliant foil thrust bearings for high speed turbine expander [J]. Journal of Xi'an Jiaotong University, 2012, 46(11): 49-52, 111.

王伟, 李晓疆, 曾强, 等. 高速透平机械全金属鼓泡箔片动压气体轴承稳定性研究 [J]. 西安交通大学学报, 2017, 51(8): 84-89.

WANG Wei, LI Xiaojiang, ZENG Qiang, et al. Stability analysis for fully hydrodynamic gas-lubricated protuberant foil bearings in high speed turbomachinery [J]. Journal of Xi'an Jiaotong University, 2017, 51(8): 84-89.

ZHENG Yueqing, LAI Tianwei, CHEN Shuangtao, et al. Static characteristics of six pads multilayer protuberant foil thrust bearings [J]. Proceedings of the Institution of Mechanical Engineers: Part J Journal of Engineering Tribology, 2017, 231(2): 158-164.

LAI Tianwei, GUO Yu, WANG Wei, et al. Development and application of integrated aerodynamic protuberant foil journal and thrust bearing in turboexpander [J]. International Journal of Rotating Machinery, 2017, 2017: 1-12.

LAI Tianwei, GUO Yu, ZHAO Qi, et al. Numerical and experimental studies on stability of cryogenic turbo-expander with protuberant foil gas bearings [J]. Cryogenics, 2018, 96: 62-74.

GUO Yu, HOU Yu, WANG Yu, et al. Numerical analysis of aerodynamic lubricated double-decked protuberant foil thrust bearing [J]. Journal of Advanced Mechanical Design, Systems, and Manufacturing, 2019, 13(3): JAMDSM0056.

王林忠, 侯予, 崔明现, 等. 箔片轴承结构阻尼的评价 [J]. 西安交通大学学报, 2006, 40(1): 40-44.

WANG L Z, HOU Y, CUI M X, et al. Damping evaluation of foil bearings [J]. Journal of Xi'an Jiaotong University, 2006, 40(1): 40-44.

ROGER K C P, HESHMAT H. Compliant foil bearing structural stiffness analysis: part Ⅰ theoretical model including strip and variable bump foil [J]. Journal of Tribology, 1992, 114(2): 400.

浏览量

下载量

CSCD

文章被引用时，请邮件提醒。

提交

工具集

关联资源

箔片安装位置对气体轴承性能影响的仿真分析

高声压激励下多孔金属材料的吸声性能数值计算

高速透平膨胀机临界转速的计算与分析

新型箔片动压止推气体轴承承载特性的试验研究

求解三维准静态矢量磁位的快速多极方法